Aeroelastic Analysis of Perovskite Solar cell

本项目旨在开发一种新的计算框架来研究钙钛矿太阳能电池(PSC)复合结构的气动弹性行为。PSC作为一种潜在的颠覆性空间市场进入者，因其高比功率、灵活性和低制造成本而吸引了科学界和航空航天工业。钙钛矿型太阳能电池(PSC)的发现已经成为第三代光伏设备中的一项主导突破。PSC的高比功率和灵活的固有特性减轻了卫星的有效载荷，同时增强了部署光伏系统的适应性。这些优势使革命性的PSC有资格成为当代空间面板领域的一个很好的竞争对手。近年来，新兴的钙钛矿和有机太阳能电池技术引起了研究人员的广泛关注。这种太阳能电池板应用于航天器或卫星，将节省推进剂，并为太空任务创造新的可能性。在PSC产品的运行过程中，不可预见的外部冲击时有发生，并且不可避免，严重危及实际设备的使用性能。在新型PSC走向实用化的成功航程中，研究其结构的动态力学性能和稳定性是一个迫切而必要的问题。这样的属性是空间结构设计的关键问题，也是抵御空气动力载荷的关键能力指标。相反，疏忽可能会导致复合材料的退化和损坏，危及PSC结构的使用性能和安全。因此，本研究旨在开发一种稳健的有限元框架来研究PSC组合梁、板和组合壳体结构的气动弹性性能。

This project aims to develop a novel computational framework to study the aeroelastic behaviour of perovskite solar cell (PSC) composite structures. The (PSC), as a potential disruptive space market entrant, has fascinated both the scientific community and the aerospace industry due to its high specific power, flexibility, and low fabrication cost. The perovskite solar cell (PSC) discovery has become a dominant breakthrough within third-generation photovoltaic devices. The resultant high specific power and flexible inherence of the PSC alleviate the satellite payload while strengthening the adaptability in deploying the photovoltaic system. These advantages qualify the revolutionary PSC as a good rival in the contemporary space panel sector. The emerging perovskite and organic solar cell technologies have recently attracted much attention among researchers. Applied in space crafts or satellites, such panels would save propellants and create novel possibilities for space missions. During the operation of the PSC products, the unanticipated external impacts are prevalent and inescapable, severely endangering the practical devices' serviceability. During the successful voyage towards practical deployment of the novel PSC, investigating the structure's dynamic mechanical performance and stability is an urgent and essential issue. Such an attribute represents a critical issue for space structure design and a crucial capability metric against aerodynamic loadings. On the contrary, negligence might yield composite degradation and damage, compromising the operational performance and safety of the PSC structure. Therefore, this research aims to develop a robust finite element framework to study the aeroelastic behaviour of PSC composite beams, plates and composite shell structures.